Effects of Cooling on Boundary-Layer Transition on a Hemisphere in Simulated Hypersonic Flow
- 1 December 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (12) , 1454-1461
- https://doi.org/10.2514/8.9868
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- The Relation Between Wall Temperature and the Effect of Roughness on Boundary-Layer TransitionJournal of the Aerospace Sciences, 1961
- Boundary-Layer Transition on Blunt Bodies with Highly Cooled Boundary LayersJournal of the Aerospace Sciences, 1960
- Note on the Stabilizing Effect of Centrifugal Forces on the Laminar Boundary Layer over Convex SurfacesJournal of the Aerospace Sciences, 1958
- Experiments on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- On Transition Experiments at Moderate Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Space-time double correlations and spectra in a turbulent boundary layerJournal of Fluid Mechanics, 1957